#	Burn time	DV	Dt	a
T1T3	2020-10-06 17:00:00.000	11.3	186.029	0.06
T1T3	2020-10-08 22:50:00.000	4.4	80.806	0.05
T1P1	2020-10-13 17:00:00.000	1.1	19.226	0.06
T1P2	2020-10-17 17:00:00.000	0.5	10.079	0.05

The table shows the maneuvers performed during this phase.
Graphs and calculations are based on NAIF's data files published on 19-Oct-2020 14:09.

#	Burn time	DV
1	2020-09-06 14:11:07.014	308.7
2	2020-09-13 14:11:06.945	293.9
3	2020-09-20 14:10:59.380	335.0
4	2020-09-27 14:10:06.491	155.6
5	2020-10-03 06:03:35.233	148.9
6	2020-10-10 06:04:11.258	94.2

Here are the impulsive micro-maneuvers obtained from the NAIF's data file.
The column "DV" shows the variation of the inertial orbital velocity expressed in µm/s.

Here's the spacecraft trajectory from August 31 to October 20 in the Bennu-centric mean ecliptic and equinox of J2000 reference frame.

The popup label shows the date, the radius vector (m), the altitude above Bennu (m), the spacecraft inertial speed (Vi, mm/s) and the speed relative to the surface of Bennu (Vs, mm/s).

Here's the same graph as above, but in the Bennu-centric Sun-North reference frame.

Instead of the inertial speed, the popup label shows the spacecraft speed in the Bennu-fixed rotating frame (Vbfr, mm/s).